NEONSAT-1A, 67614
Orbit data source: Space-Track
NEONSAT-1A, 67614 is a payload satellite owned by KAIST (KR) in SSO that was launched on Fri, 30 Jan 2026 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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67614 intel report (Beta)
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Identifier
Orbit
Country
KR / 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, 14.5 m
Radar Cross Section
0.625 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 NEONSAT-1A
1 67614U 26019A 26171.28776823 .00002843 00000-0 18623-3 0 9992
2 67614 97.4271 291.3546 0013306 176.0427 184.0910 15.08440907 21280Epoch: 2026-06-20T06:54Z
TLE epoch observation values (Epoch: 2026-06-20T06:54:23.175Z)
Latitude
0.00006°
Longitude
-80.74652°
Altitude
553.223 km
Speed
7.58 km/s
True Right ascension
19h 25m 25s
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
07:24:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
547.148 km
Perigee altitude
528.743 km
Semi-major axis
6,916.083 km
Eccentricity
0.00133
Inclination
97.4271°
RAAN
291.3546°
Arg. of periapsis
176.0427°
True anomaly
184.08014°
Mean anomaly
184.091°
Eccentric anomaly
184.08557°
Mean motion
3.77357 °/min
Orbital period
95.4 mins
BSTAR
0.00018623
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Other satellites on launch #19 in the year 2026 (2026-01-30 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-1A 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-20 21:48:20.751Z | 328.999° NNW | 2026-06-20 21:50:20.751Z | 291.455° WNW | 18.714° | 2026-06-20 21:52:20.751Z | 253.754° W |
| 5 mins | 2026-06-21 08:31:20.751Z | 206.696° SW | 2026-06-21 08:33:20.751Z | 267.804° W | 33.014° | 2026-06-21 08:36:20.751Z | 329.583° NNW |
| 4 mins | 2026-06-21 20:07:20.751Z | 62.917° ENE | 2026-06-21 20:08:20.751Z | 83.447° E | 20.182° | 2026-06-21 20:11:20.751Z | 141.947° SSE |
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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