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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
7 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 7 hours ago
0 NEONSAT-1
1 59587U 24077A   25114.89734940  .00016984  00000-0  61949-3 0  9991
2 59587  97.3800 195.6984 0012901  87.0149 273.2567 15.28145230 55651
Epoch: 2025-04-24T21:32Z
Definitive object data (Epoch: 2025-04-24T21:32:10.988Z)
Latitude
0.00002°
Longitude
19.49042°
Altitude
483.968 km
Speed
7.624 km/s
True Right ascension
13h 02m 47s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at TLE epoch
Visualization TLE readout
Latitude
82.64616°
Longitude
-73.80951°
Altitude
486.067 km
Speed
7.634 km/s
Apparent Right ascension
00h 06m 58s
Apparent Declination
30° 14' 11"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
11:26:14
Azimuth
350.691° N
Elevation
-19.213°
Doppler factor
1
Orbital elements
Apogee altitude
487.156 km
Perigee altitude
469.465 km
Semi-major axis
6,856.448 km
Eccentricity
0.0012901
Inclination
97.38°
RAAN
195.6984°
Arg. of periapsis
87.0149°
True anomaly
273.10909°
Mean anomaly
273.2567°
Eccentric anomaly
273.1829°
Mean motion
3.82291 °/min
BSTAR
0.00061949
Orbital period
94.17 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.
6 mins2025-04-25 05:30:58.296Z175.77° S2025-04-25 05:33:58.296Z244.467° WSW42.785°2025-04-25 05:36:58.296Z341.47° N
5 mins2025-04-25 18:31:58.296Z353.212° N2025-04-25 18:33:58.296Z301.26° NW35.956°2025-04-25 18:36:58.296Z214.087° SW
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