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
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 26052.59269563 .00011317 00000-0 46501-3 0 9995
2 43784 97.4036 108.1436 0002418 8.6550 351.4729 15.24348154395699Epoch: 2026-02-21T14:13Z
TLE epoch observation values (Epoch: 2026-02-21T14:13:28.902Z)
Latitude
0°
Longitude
103.26011°
Altitude
494.196 km
Speed
7.619 km/s
True Right ascension
07h 12m 34s
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
23:38:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
491.364 km
Perigee altitude
488.043 km
Semi-major axis
6,867.84 km
Eccentricity
0.00024
Inclination
97.4036°
RAAN
108.1436°
Arg. of periapsis
8.655°
True anomaly
351.46879°
Mean anomaly
351.4729°
Eccentric anomaly
351.47085°
Mean motion
3.8134 °/min
Orbital period
94.4 mins
BSTAR
0.00046501
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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 | 2026-02-22 02:58:14.644Z | 122.953° SE | 2026-02-22 03:01:14.644Z | 58.641° ENE | 22.419° | 2026-02-22 03:03:14.644Z | 20.273° NNE |
| 4 mins | 2026-02-22 16:01:14.644Z | 50.361° ENE | 2026-02-22 16:03:14.644Z | 114.945° SE | 28.925° | 2026-02-22 16:05:14.644Z | 157.877° S |
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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