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 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 shape, 14.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 NEONSAT-1A
1 67614U 26019A 26078.86644339 .00002986 00000-0 19826-3 0 9992
2 67614 97.4137 202.0825 0014520 134.9205 225.3204 15.07882963 7354Epoch: 2026-03-19T20:47Z
TLE epoch observation values (Epoch: 2026-03-19T20:47:40.708Z)
Latitude
-0.00009°
Longitude
72.75318°
Altitude
552.819 km
Speed
7.581 km/s
True Right ascension
13h 28m 19s
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
11:50:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
549.697 km
Perigee altitude
529.608 km
Semi-major axis
6,917.79 km
Eccentricity
0.00145
Inclination
97.4137°
RAAN
202.0825°
Arg. of periapsis
134.9205°
True anomaly
225.20224°
Mean anomaly
225.3204°
Eccentric anomaly
225.26131°
Mean motion
3.77218 °/min
Orbital period
95.44 mins
BSTAR
0.00019826
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-20 08:03:49.625Z | 160.467° S | 2026-03-20 08:07:49.625Z | 21.816° NNE | 41.806° | 2026-03-20 08:10:49.625Z | 352.466° N |
| 5 mins | 2026-03-20 21:15:49.625Z | 356.166° N | 2026-03-20 21:17:49.625Z | 290.269° WNW | 40.584° | 2026-03-20 21:20:49.625Z | 208.141° SW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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