SNUGLITE, 43784
Orbit data source: Space-Track
SNUGLITE, 43784 is a payload satellite owned by SNU (KR) in SSO that was launched on Mon, 03 Dec 2018 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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43784 intel report (Beta)
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Identifier
Orbit
Country
KR / SKORRelated business
Manufacturer
SNU
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 2U, Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Rod, 0.2 m
Radar Cross Section
0.025 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 SNUGLITE
1 43784U 18099AC 26071.10098358 .00012909 00000-0 52115-3 0 9991
2 43784 97.4003 126.4343 0001419 262.3882 97.7195 15.24908542398514Epoch: 2026-03-12T02:25Z
TLE epoch observation values (Epoch: 2026-03-12T02:25:24.981Z)
Latitude
0.00002°
Longitude
-79.6755°
Altitude
494.288 km
Speed
7.618 km/s
True Right ascension
08h 25m 44s
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
16:24:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.993 km
Perigee altitude
487.045 km
Semi-major axis
6,866.156 km
Eccentricity
0.00014
Inclination
97.4003°
RAAN
126.4343°
Arg. of periapsis
262.3882°
True anomaly
97.73561°
Mean anomaly
97.7195°
Eccentric anomaly
97.72756°
Mean motion
3.81481 °/min
Orbital period
94.37 mins
BSTAR
0.00052115
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Other satellites on launch #99 in the year 2018 (2018-12-03 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.SNUGLITE 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 | 2026-03-12 15:36:37.683Z | 60.343° ENE | 2026-03-12 15:38:37.683Z | 99.33° ESE | 16.533° | 2026-03-12 15:40:37.683Z | 134.653° SE |
| 4 mins | 2026-03-12 17:10:37.683Z | 323.11° NNW | 2026-03-12 17:11:37.683Z | 298.118° NW | 23.389° | 2026-03-12 17:14:37.683Z | 234.62° WSW |
| 5 mins | 2026-03-13 03:45:37.683Z | 175.166° S | 2026-03-13 03:47:37.683Z | 229.344° WSW | 43.848° | 2026-03-13 03:50:37.683Z | 343.534° N |
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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