Showing default

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.

Loading next visibility...
Identifier
59587, 2024-077A
Orbit
SSO
Country
Flag of KRKR / SKOR
Related business
Manufacturer
KAIST/SATRHW
Mission
Operational Civil Imaging
Bus & Motor
NEONSAT, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
2024-04-23 (2 years ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + Cyl + 4 Pan, 0.6 m
Radar Cross Section
0.625 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago
0 NEONSAT-1
1 59587U 24077A   26254.65426807  .00010957  00000-0  27228-3 0  9997
2 59587  97.3456 338.9609 0009160  83.1896 277.0392 15.40444781133037
Epoch: 2026-09-11T15:42Z
TLE epoch observation values (Epoch: 2026-09-11T15:42:08.761Z)
Latitude
-0.00004°
Longitude
112.74988°
Altitude
447.155 km
Speed
7.644 km/s
True Right ascension
22h 35m 50s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
12:35:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
447.979 km
Perigee altitude
435.485 km
Semi-major axis
6,819.869 km
Eccentricity
0.00092
Inclination
97.3456°
RAAN
338.9609°
Arg. of periapsis
83.1896°
True anomaly
276.93501°
Mean anomaly
277.0392°
Eccentric anomaly
276.98711°
Mean motion
3.85371 °/min
Orbital period
93.42 mins
BSTAR
0.00027228
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #77 in the year 2024 (2024-04-23 UTC)

Documentation

Showing up to 5 results
|