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: 1 day ago
TLE from 1 day ago
0 SNUSAT-2
1 43782U 18099AA 25341.12233835 .00013749 00000-0 67567-3 0 9991
2 43782 97.4356 32.6257 0009782 244.3568 115.6656 15.18119445383859Epoch: 2025-12-07T02:56Z
TLE epoch observation values (Epoch: 2025-12-07T02:56:10.033Z)
Latitude
-0.00001°
Longitude
-87.55636°
Altitude
517.536 km
Speed
7.603 km/s
True Right ascension
02h 10m 30s
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
00:45:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
515.231 km
Perigee altitude
501.758 km
Semi-major axis
6,886.631 km
Eccentricity
0.00098
Inclination
97.4356°
RAAN
32.6257°
Arg. of periapsis
244.3568°
True anomaly
115.76658°
Mean anomaly
115.6656°
Eccentric anomaly
115.7161°
Mean motion
3.79781 °/min
Orbital period
94.79 mins
BSTAR
0.00067567
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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 | 2025-12-08 02:48:52.061Z | 113.325° SE | 2025-12-08 02:50:52.061Z | 77.432° E | 19.393° | 2025-12-08 02:53:52.061Z | 21.797° NNE |
| 4 mins | 2025-12-08 04:23:52.061Z | 235.634° WSW | 2025-12-08 04:24:52.061Z | 259.501° W | 22.1° | 2025-12-08 04:27:52.061Z | 317.327° NNW |
| 4 mins | 2025-12-08 15:54:52.061Z | 56.892° ENE | 2025-12-08 15:55:52.061Z | 82.264° E | 26.019° | 2025-12-08 15:58:52.061Z | 153.121° SSE |
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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