Showing default

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.

Loading next visibility...
Identifier
43782, 2018-099AA
Orbit
SSO
Country
Flag of KRKR / SKOR
Related business
Manufacturer
SNU
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
2018-12-03 (7 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 SNUSAT-2
1 43782U 18099AA  26126.11106903  .00008774  00000-0  39556-3 0  9996
2 43782  97.4086 180.1552 0011997  85.9906 274.2701 15.21200438406634
Epoch: 2026-05-06T02:39Z
TLE epoch observation values (Epoch: 2026-05-06T02:39:56.364Z)
Latitude
Longitude
-83.80591°
Altitude
504.706 km
Speed
7.612 km/s
True Right ascension
12h 00m 37s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
13:23:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.434 km
Perigee altitude
490.932 km
Semi-major axis
6,877.32 km
Eccentricity
0.0012
Inclination
97.4086°
RAAN
180.1552°
Arg. of periapsis
85.9906°
True anomaly
274.13299°
Mean anomaly
274.2701°
Eccentric anomaly
274.20155°
Mean motion
3.80552 °/min
Orbital period
94.6 mins
BSTAR
0.00039556
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|