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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68482 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
Spire/Glasgow
Mission
Operational spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
11 kg wet, 11 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 LEMUR-2 SEJONG-3
1 68482U 26067BU 26171.34971815 .00002835 00000-0 27852-3 0 9999
2 68482 97.7568 129.6510 0001879 217.7228 142.3860 14.92951381 12202Epoch: 2026-06-20T08:23Z
TLE epoch observation values (Epoch: 2026-06-20T08:23:35.648Z)
Latitude
0°
Longitude
95.18686°
Altitude
592.819 km
Speed
7.563 km/s
True Right ascension
08h 38m 36s
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
07:11:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.064 km
Perigee altitude
584.447 km
Semi-major axis
6,963.893 km
Eccentricity
0.00019
Inclination
97.7568°
RAAN
129.651°
Arg. of periapsis
217.7228°
True anomaly
142.39914°
Mean anomaly
142.386°
Eccentric anomaly
142.39257°
Mean motion
3.73478 °/min
Orbital period
96.39 mins
BSTAR
0.00027852
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.LEMUR-2 SEJONG-3 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 | 2026-06-20 21:23:13.821Z | 174.612° S | 2026-06-20 21:26:13.821Z | 234.179° WSW | 43.52° | 2026-06-20 21:30:13.821Z | 343.226° N |
| 6 mins | 2026-06-21 10:42:13.821Z | 344.657° N | 2026-06-21 10:45:13.821Z | 272.121° WNW | 29.329° | 2026-06-21 10:48:13.821Z | 224.111° SW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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