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: 6 hours ago
TLE from 6 hours ago
0 SNUGLITE
1 43784U 18099AC 25286.26435844 .00018177 00000-0 83951-3 0 9995
2 43784 97.4262 338.5983 0004819 85.1514 275.0272 15.20243286375714Epoch: 2025-10-13T06:20Z
TLE epoch observation values (Epoch: 2025-10-13T06:20:40.569Z)
Latitude
0.00006°
Longitude
-138.64038°
Altitude
507.907 km
Speed
7.61 km/s
True Right ascension
22h 34m 23s
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
07:04:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.388 km
Perigee altitude
498.757 km
Semi-major axis
6,880.21 km
Eccentricity
0.00048
Inclination
97.4262°
RAAN
338.5983°
Arg. of periapsis
85.1514°
True anomaly
274.97219°
Mean anomaly
275.0272°
Eccentric anomaly
274.99969°
Mean motion
3.80313 °/min
Orbital period
94.66 mins
BSTAR
0.00083951
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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 | 2025-10-13 16:23:15.556Z | 16.418° NNE | 2025-10-13 16:26:15.556Z | 125.711° SE | 44.001° | 2025-10-13 16:29:15.556Z | 187.276° SSW |
| 4 mins | 2025-10-14 03:02:15.556Z | 113.588° SE | 2025-10-14 03:04:15.556Z | 60.924° ENE | 24.88° | 2025-10-14 03:06:15.556Z | 19.506° 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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