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: 7 hours ago
TLE from 7 hours ago
0 NEONSAT-1A
1 67614U 26019A 26032.93938282 .00004767 00000-0 31747-3 0 9998
2 67614 97.4098 157.8088 0011896 300.1094 59.8954 15.07513442 431Epoch: 2026-02-01T22:32Z
TLE epoch observation values (Epoch: 2026-02-01T22:32:42.675Z)
Latitude
-0.00009°
Longitude
47.48917°
Altitude
542.751 km
Speed
7.593 km/s
True Right ascension
10h 31m 14s
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
07:33:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
549.015 km
Perigee altitude
532.553 km
Semi-major axis
6,918.921 km
Eccentricity
0.00119
Inclination
97.4098°
RAAN
157.8088°
Arg. of periapsis
300.1094°
True anomaly
60.01342°
Mean anomaly
59.8954°
Eccentric anomaly
59.9544°
Mean motion
3.77125 °/min
Orbital period
95.46 mins
BSTAR
0.00031747
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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 | 2026-02-02 08:13:12.934Z | 165.754° S | 2026-02-02 08:17:12.934Z | 358.35° N | 43.889° | 2026-02-02 08:20:12.934Z | 348.939° N |
| 6 mins | 2026-02-02 21:25:12.934Z | 354.058° N | 2026-02-02 21:27:12.934Z | 312.372° NW | 36.072° | 2026-02-02 21:31:12.934Z | 211.468° 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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