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 spacecraft
Bus & Motor
NEONSAT, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 NEONSAT-1
1 59587U 24077A 25258.31316275 .00014143 00000-0 47931-3 0 9994
2 59587 97.3730 337.9897 0009614 297.4932 62.5331 15.30624086 77578Epoch: 2025-09-15T07:30Z
TLE epoch observation values (Epoch: 2025-09-15T07:30:57.261Z)
Latitude
-0.00006°
Longitude
-129.26849°
Altitude
474.021 km
Speed
7.631 km/s
True Right ascension
22h 31m 57s
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
11:01:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.484 km
Perigee altitude
464.315 km
Semi-major axis
6,849.036 km
Eccentricity
0.00096
Inclination
97.373°
RAAN
337.9897°
Arg. of periapsis
297.4932°
True anomaly
62.6309°
Mean anomaly
62.5331°
Eccentric anomaly
62.582°
Mean motion
3.82912 °/min
Orbital period
94.02 mins
BSTAR
0.00047931
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-15 19:03:17.934Z | 338.177° N | 2025-09-15 19:06:17.934Z | 277.741° WNW | 19.353° | 2025-09-15 19:08:17.934Z | 242.058° WSW |
| 5 mins | 2025-09-16 05:37:17.934Z | 182.093° SSW | 2025-09-16 05:39:17.934Z | 257.455° W | 42.181° | 2025-09-16 05:42:17.934Z | 340.625° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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