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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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Identifier
59587, 2024-077A
Orbit
SSO
Last TLE update
8 hours ago
Origin
Manufacturer
KAIST/SATRHW
Mission
Operational spacecraft
Bus & Motor
NEONSAT, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
2024-04-23 (1 year ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
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 8 hours ago
0 NEONSAT-1
1 59587U 24077A   25128.90846369  .00009724  00000-0  35234-3 0  9999
2 59587  97.3795 209.5814 0012193  41.6546 318.5620 15.28508046 57799
Epoch: 2025-05-08T21:48Z
Definitive object data (Epoch: 2025-05-08T21:48:11.262Z)
Latitude
-0.00006°
Longitude
15.56227°
Altitude
477.108 km
Speed
7.631 km/s
True Right ascension
13h 58m 19s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at TLE epoch
Visualization TLE readout
Latitude
34.83596°
Longitude
-158.94459°
Altitude
487.087 km
Speed
7.624 km/s
Apparent Right ascension
02h 23m 02s
Apparent Declination
0° 55' 20"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
14:26:12
Azimuth
1.255° NNE
Elevation
-51°
Doppler factor
1
Orbital elements
Apogee altitude
485.584 km
Perigee altitude
468.866 km
Semi-major axis
6,855.362 km
Eccentricity
0.0012193
Inclination
97.3795°
RAAN
209.5814°
Arg. of periapsis
41.6546°
True anomaly
318.46943°
Mean anomaly
318.562°
Eccentric anomaly
318.51572°
Mean motion
3.82382 °/min
BSTAR
0.00035234
Orbital period
94.15 mins
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Other satellites on launch #77 in the year 2024 (2024-04-23 UTC)

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.
4 mins2025-05-09 18:48:23.425Z327.036° NNW2025-05-09 18:49:23.425Z299.621° NW26.164°2025-05-09 18:52:23.425Z229.758° WSW
5 mins2025-05-10 05:22:23.425Z163.682° S2025-05-10 05:24:23.425Z5.901° NNE43.738°2025-05-10 05:27:23.425Z349.505° N
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