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LEMUR-2 SEJONG-3, 68482

Orbit data source: Space-Track

LEMUR-2 SEJONG-3, 68482 is a payload satellite owned by Hancom InSpace (DE) in SSO that was launched on Mon, 30 Mar 2026 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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Identifier
68482, 2026-067BU
Orbit
SSO
Country
Flag of DEDE / GER
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
11 kg wet, 11 kg dry
Launch date (UTC)
2026-03-30 (4 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.077 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 LEMUR-2 SEJONG-3
1 68482U 26067BU  26220.13756380  .00001265  00000-0  12643-3 0  9997
2 68482  97.7600 177.7780 0005103  80.9123 279.2673 14.93232262 19480
Epoch: 2026-08-08T03:18Z
TLE epoch observation values (Epoch: 2026-08-08T03:18:05.512Z)
Latitude
-0.00009°
Longitude
171.60182°
Altitude
590.338 km
Speed
7.565 km/s
True Right ascension
11h 51m 06s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
00:48:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.435 km
Perigee altitude
581.329 km
Semi-major axis
6,963.019 km
Eccentricity
0.00051
Inclination
97.76°
RAAN
177.778°
Arg. of periapsis
80.9123°
True anomaly
279.20958°
Mean anomaly
279.2673°
Eccentric anomaly
279.23844°
Mean motion
3.73548 °/min
Orbital period
96.37 mins
BSTAR
0.00012643
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