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: 22 hours ago
TLE from 22 hours ago
0 SNUGLITE
1 43784U 18099AC 25339.08855405 .00024698 00000-0 10822-2 0 9994
2 43784 97.4182 30.6475 0001819 238.6373 121.4686 15.21994956383749Epoch: 2025-12-05T02:07Z
TLE epoch observation values (Epoch: 2025-12-05T02:07:31.069Z)
Latitude
0.00001°
Longitude
-75.36762°
Altitude
503.57 km
Speed
7.612 km/s
True Right ascension
02h 02m 35s
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
22:15:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.038 km
Perigee altitude
495.537 km
Semi-major axis
6,874.925 km
Eccentricity
0.00018
Inclination
97.4182°
RAAN
30.6475°
Arg. of periapsis
238.6373°
True anomaly
121.48638°
Mean anomaly
121.4686°
Eccentric anomaly
121.47749°
Mean motion
3.80751 °/min
Orbital period
94.55 mins
BSTAR
0.0010822
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Other satellites on launch #99 in the year 2018 (2018-12-03 UTC)
Did you know?
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 | 2025-12-06 03:30:09.274Z | 157.138° SSE | 2025-12-06 03:33:09.274Z | 49.032° ENE | 42.457° | 2025-12-06 03:36:09.274Z | 354.074° N |
| 5 mins | 2025-12-06 16:34:09.274Z | 6.596° NNE | 2025-12-06 16:36:09.274Z | 309.741° NW | 44.176° | 2025-12-06 16:39:09.274Z | 198.316° SSW |
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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