SNUSAT-2, 43782
Orbit data source: Space-Track
SNUSAT-2, 43782 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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43782 intel report (Beta)
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Identifier
Orbit
Country
KR / SKORRelated business
Manufacturer
SNU
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 SNUSAT-2
1 43782U 18099AA 26215.59849001 .00008346 00000-0 36214-3 0 9993
2 43782 97.4019 268.2666 0011726 125.4627 234.7706 15.22528651420244Epoch: 2026-08-03T14:21Z
TLE epoch observation values (Epoch: 2026-08-03T14:21:49.536Z)
Latitude
-0.00002°
Longitude
100.63091°
Altitude
505.969 km
Speed
7.609 km/s
True Right ascension
17h 53m 03s
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
23:13:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.238 km
Perigee altitude
487.119 km
Semi-major axis
6,873.316 km
Eccentricity
0.00117
Inclination
97.4019°
RAAN
268.2666°
Arg. of periapsis
125.4627°
True anomaly
234.66093°
Mean anomaly
234.7706°
Eccentric anomaly
234.71576°
Mean motion
3.80885 °/min
Orbital period
94.52 mins
BSTAR
0.00036214
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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.SNUSAT-2 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 | 2026-08-05 15:50:21.219Z | 45.512° ENE | 2026-08-05 15:52:21.219Z | 89.204° E | 24.567° | 2026-08-05 15:55:21.219Z | 153.641° SSE |
| 5 mins | 2026-08-06 04:01:21.219Z | 204.236° SW | 2026-08-06 04:03:21.219Z | 273.983° WNW | 33.422° | 2026-08-06 04:06:21.219Z | 332.596° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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