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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 (1 year 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, Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 XCUBE-1
1 62400U 24247Z   26041.01823613  .00009814  00000-0  36960-3 0  9997
2 62400  44.9978 267.7325 0005573 190.2600 169.8170 15.27377160 63500
Epoch: 2026-02-10T00:26Z
TLE epoch observation values (Epoch: 2026-02-10T00:26:15.601Z)
Latitude
-0.00002°
Longitude
121.06275°
Altitude
487.418 km
Speed
7.621 km/s
True Right ascension
17h 50m 55s
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
09:14:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.091 km
Perigee altitude
481.441 km
Semi-major axis
6,863.403 km
Eccentricity
0.00056
Inclination
44.9978°
RAAN
267.7325°
Arg. of periapsis
190.26°
True anomaly
169.82828°
Mean anomaly
169.817°
Eccentric anomaly
169.82264°
Mean motion
3.8171 °/min
Orbital period
94.31 mins
BSTAR
0.0003696
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Documentation

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