Showing default

LILIUM-2, 66679

Orbit data source: Space-Track

LILIUM-2, 66679 is a payload satellite owned by NCKU (TW) in SSO that was launched on Fri, 28 Nov 2025 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
66679, 2025-276P
Orbit
SSO
Country
Flag of TWTW / TWN
Related business
Manufacturer
Satoro
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
2025-11-28 (9 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 LILIUM-2
1 66679U 25276P   26238.63459369  .00003002  00000-0  14973-3 0  9994
2 66679  97.4109 310.2598 0007523 115.1167 245.0848 15.18266824 41080
Epoch: 2026-08-26T15:13Z
TLE epoch observation values (Epoch: 2026-08-26T15:13:48.894Z)
Latitude
-0.00009°
Longitude
106.92132°
Altitude
516.353 km
Speed
7.604 km/s
True Right ascension
20h 41m 02s
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
17:12:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.227 km
Perigee altitude
502.866 km
Semi-major axis
6,886.184 km
Eccentricity
0.00075
Inclination
97.4109°
RAAN
310.2598°
Arg. of periapsis
115.1167°
True anomaly
245.00665°
Mean anomaly
245.0848°
Eccentric anomaly
245.04572°
Mean motion
3.79818 °/min
Orbital period
94.78 mins
BSTAR
0.00014973
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
|