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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 (10 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, 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   25301.55243708  .00010631  00000-0  42987-3 0  9990
2 62400  44.9921 116.8095 0007029 269.9021  90.1056 15.24917514 47540
Epoch: 2025-10-28T13:15Z
TLE epoch observation values (Epoch: 2025-10-28T13:15:30.563Z)
Latitude
0.00001°
Longitude
-119.20612°
Altitude
491.043 km
Speed
7.621 km/s
True Right ascension
07h 47m 14s
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
11:35:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.471 km
Perigee altitude
487.812 km
Semi-major axis
6,870.779 km
Eccentricity
0.0007
Inclination
44.9921°
RAAN
116.8095°
Arg. of periapsis
269.9021°
True anomaly
90.18615°
Mean anomaly
90.1056°
Eccentric anomaly
90.14587°
Mean motion
3.81096 °/min
Orbital period
94.46 mins
BSTAR
0.00042987
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