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XCUBE-1, 62400

Orbit data source: Space-Track

XCUBE-1, 62400 is an American payload satellite in LEO that was launched on Sat, 21 Dec 2024 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
62400, 2024-247Z
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
EXOBOT
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
2024-12-21 (8 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, 0.6 m
Radar Cross Section
0.138 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 XCUBE-1
1 62400U 24247Z   25241.25609691  .00008470  00000-0  35935-3 0  9990
2 62400  44.9965  84.3233 0004374 272.9502  87.0879 15.23541505 38347
Epoch: 2025-08-29T06:08Z
TLE epoch observation values (Epoch: 2025-08-29T06:08:46.773Z)
Latitude
0.00001°
Longitude
14.42107°
Altitude
495.015 km
Speed
7.619 km/s
True Right ascension
05h 37m 17s
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
14:10:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.783 km
Perigee altitude
493.768 km
Semi-major axis
6,874.912 km
Eccentricity
0.00044
Inclination
44.9965°
RAAN
84.3233°
Arg. of periapsis
272.9502°
True anomaly
87.13796°
Mean anomaly
87.0879°
Eccentric anomaly
87.11293°
Mean motion
3.80752 °/min
Orbital period
94.55 mins
BSTAR
0.00035935
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