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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 NEONSAT-1A
1 67614U 26019A 26039.84235935 .00003451 00000-0 23057-3 0 9994
2 67614 97.4084 164.4603 0011951 273.5611 86.4250 15.07575901 1471Epoch: 2026-02-08T20:12Z
TLE epoch observation values (Epoch: 2026-02-08T20:12:59.847Z)
Latitude
-0.00009°
Longitude
82.26522°
Altitude
546.177 km
Speed
7.589 km/s
True Right ascension
10h 57m 50s
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
10:15:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
548.861 km
Perigee altitude
532.324 km
Semi-major axis
6,918.729 km
Eccentricity
0.0012
Inclination
97.4084°
RAAN
164.4603°
Arg. of periapsis
273.5611°
True anomaly
86.56169°
Mean anomaly
86.425°
Eccentric anomaly
86.49335°
Mean motion
3.77141 °/min
Orbital period
95.46 mins
BSTAR
0.00023057
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-09 09:05:44.342Z | 224.215° SW | 2026-02-09 09:07:44.342Z | 261.38° W | 19.951° | 2026-02-09 09:10:44.342Z | 314.241° NW |
| 5 mins | 2026-02-09 20:41:44.342Z | 35.698° NE | 2026-02-09 20:43:44.342Z | 86.218° E | 34.713° | 2026-02-09 20:46:44.342Z | 166.311° S |
| 4 mins | 2026-02-10 07:25:44.342Z | 98.624° ESE | 2026-02-10 07:26:44.342Z | 78.101° E | 20.315° | 2026-02-10 07:29:44.342Z | 22.452° NNE |
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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