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: 16 hours ago
TLE from 16 hours ago
0 SNUGLITE
1 43784U 18099AC 25324.62224781 .00011702 00000-0 52215-3 0 9990
2 43784 97.4201 16.3855 0002148 326.2673 33.8426 15.21537828381542Epoch: 2025-11-20T14:56Z
TLE epoch observation values (Epoch: 2025-11-20T14:56:02.210Z)
Latitude
-0.00004°
Longitude
92.49931°
Altitude
503.066 km
Speed
7.613 km/s
True Right ascension
01h 05m 32s
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
04:07:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.643 km
Perigee altitude
496.689 km
Semi-major axis
6,876.303 km
Eccentricity
0.00021
Inclination
97.4201°
RAAN
16.3855°
Arg. of periapsis
326.2673°
True anomaly
33.85631°
Mean anomaly
33.8426°
Eccentric anomaly
33.84946°
Mean motion
3.80637 °/min
Orbital period
94.58 mins
BSTAR
0.00052215
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-21 16:44:35.238Z | 0.675° NNE | 2025-11-21 16:47:35.238Z | 297.885° NW | 38.437° | 2025-11-21 16:50:35.238Z | 211.173° SW |
| 5 mins | 2025-11-22 03:22:35.238Z | 145.407° SSE | 2025-11-22 03:24:35.238Z | 97.114° ESE | 37.583° | 2025-11-22 03:27:35.238Z | 2.101° NNE |
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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