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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 SNUSAT-2
1 43782U 18099AA 25260.12528111 .00007248 00000-0 37998-3 0 9997
2 43782 97.4503 313.0872 0012434 161.8761 198.2918 15.16005712371571Epoch: 2025-09-17T03:00Z
TLE epoch observation values (Epoch: 2025-09-17T03:00:24.287Z)
Latitude
-0°
Longitude
-88.31972°
Altitude
529.155 km
Speed
7.594 km/s
True Right ascension
20h 52m 20s
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
13:24:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
523.471 km
Perigee altitude
506.329 km
Semi-major axis
6,893.037 km
Eccentricity
0.00124
Inclination
97.4503°
RAAN
313.0872°
Arg. of periapsis
161.8761°
True anomaly
198.24715°
Mean anomaly
198.2918°
Eccentric anomaly
198.26947°
Mean motion
3.79251 °/min
Orbital period
94.92 mins
BSTAR
0.00037998
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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 | 2025-09-18 02:54:25.803Z | 123.452° SE | 2025-09-18 02:57:25.803Z | 68.685° E | 22.055° | 2025-09-18 02:59:25.803Z | 27.015° NE |
| 5 mins | 2025-09-18 16:01:25.803Z | 41.463° NE | 2025-09-18 16:03:25.803Z | 92.312° ESE | 30.224° | 2025-09-18 16:06:25.803Z | 161.841° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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