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: 12 hours ago
TLE from 12 hours ago
0 SNUSAT-2
1 43782U 18099AA 25291.13908436 .00015521 00000-0 78998-3 0 9992
2 43782 97.4453 343.5305 0012873 65.7329 294.5248 15.16831140376273Epoch: 2025-10-18T03:20Z
TLE epoch observation values (Epoch: 2025-10-18T03:20:16.888Z)
Latitude
-0°
Longitude
-93.41426°
Altitude
514.835 km
Speed
7.608 km/s
True Right ascension
22h 54m 07s
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
10:35:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
521.267 km
Perigee altitude
503.527 km
Semi-major axis
6,890.534 km
Eccentricity
0.00129
Inclination
97.4453°
RAAN
343.5305°
Arg. of periapsis
65.7329°
True anomaly
294.39051°
Mean anomaly
294.5248°
Eccentric anomaly
294.45766°
Mean motion
3.79458 °/min
Orbital period
94.87 mins
BSTAR
0.00078998
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-18 16:33:20.103Z | 8.99° NNE | 2025-10-18 16:37:20.103Z | 224.033° SW | 42.689° | 2025-10-18 16:40:20.103Z | 197.727° SSW |
| 5 mins | 2025-10-19 03:14:20.103Z | 127.738° SE | 2025-10-19 03:16:20.103Z | 63.343° ENE | 32.241° | 2025-10-19 03:19:20.103Z | 4.967° NNE |
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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