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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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: 13 hours ago
TLE from 13 hours ago
0 SNUGLITE
1 43784U 18099AC 25255.91028809 .00007168 00000-0 34310-3 0 9995
2 43784 97.4313 308.7237 0004020 161.0016 199.1369 15.19254603371102Epoch: 2025-09-12T21:50Z
TLE epoch observation values (Epoch: 2025-09-12T21:50:48.89Z)
Latitude
-0.00009°
Longitude
-11.13122°
Altitude
513.797 km
Speed
7.605 km/s
True Right ascension
20h 34m 53s
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
03:38:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.827 km
Perigee altitude
502.293 km
Semi-major axis
6,883.197 km
Eccentricity
0.0004
Inclination
97.4313°
RAAN
308.7237°
Arg. of periapsis
161.0016°
True anomaly
199.12181°
Mean anomaly
199.1369°
Eccentric anomaly
199.12935°
Mean motion
3.80065 °/min
Orbital period
94.72 mins
BSTAR
0.0003431
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-13 15:48:32.347Z | 42.716° NE | 2025-09-13 15:51:32.347Z | 105.918° ESE | 23.053° | 2025-09-13 15:53:32.347Z | 145.997° SSE |
| 5 mins | 2025-09-14 04:01:32.347Z | 202.751° SW | 2025-09-14 04:03:32.347Z | 277.056° WNW | 34.742° | 2025-09-14 04:06:32.347Z | 333.812° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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