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: 16 hours ago
TLE from 16 hours ago
0 SNUSAT-2
1 43782U 18099AA 25299.12072285 .00009676 00000-0 49133-3 0 9996
2 43782 97.4419 351.3675 0012240 40.3765 319.8374 15.17038799377488Epoch: 2025-10-26T02:53Z
TLE epoch observation values (Epoch: 2025-10-26T02:53:50.454Z)
Latitude
-0.00008°
Longitude
-86.83419°
Altitude
511.436 km
Speed
7.612 km/s
True Right ascension
23h 25m 28s
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
14:17:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
520.2 km
Perigee altitude
503.334 km
Semi-major axis
6,889.904 km
Eccentricity
0.00122
Inclination
97.4419°
RAAN
351.3675°
Arg. of periapsis
40.3765°
True anomaly
319.74683°
Mean anomaly
319.8374°
Eccentric anomaly
319.79213°
Mean motion
3.7951 °/min
Orbital period
94.86 mins
BSTAR
0.00049133
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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 | 2025-10-27 02:47:23.242Z | 114.096° SE | 2025-10-27 02:50:23.242Z | 58.058° ENE | 18.026° | 2025-10-27 02:52:23.242Z | 24.249° NE |
| 4 mins | 2025-10-27 04:22:23.242Z | 229.908° WSW | 2025-10-27 04:23:23.242Z | 253.173° W | 22.321° | 2025-10-27 04:26:23.242Z | 316.036° NNW |
| 5 mins | 2025-10-27 15:53:23.242Z | 47.312° ENE | 2025-10-27 15:55:23.242Z | 93.811° ESE | 25.993° | 2025-10-27 15:58:23.242Z | 155.451° 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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