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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 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.138 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 XCUBE-1
1 62400U 24247Z   26235.17996337  .00005794  00000-0  20279-3 0  9992
2 62400  44.9955 285.3151 0003943 263.8441  96.1994 15.30496428 93228
Epoch: 2026-08-23T04:19Z
TLE epoch observation values (Epoch: 2026-08-23T04:19:08.835Z)
Latitude
Longitude
-110.95143°
Altitude
474.621 km
Speed
7.63 km/s
True Right ascension
19h 01m 15s
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
16:14:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.645 km
Perigee altitude
473.24 km
Semi-major axis
6,854.079 km
Eccentricity
0.00039
Inclination
44.9955°
RAAN
285.3151°
Arg. of periapsis
263.8441°
True anomaly
96.24432°
Mean anomaly
96.1994°
Eccentric anomaly
96.22186°
Mean motion
3.82489 °/min
Orbital period
94.12 mins
BSTAR
0.00020279
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Documentation

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