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CROCUBE, 62394

Orbit data source: Space-Track

CROCUBE, 62394 is a Croatian 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
62394, 2024-247T
Orbit
LEO
Country
Flag of HRHR / HRV
Related business
Manufacturer
SpaceManic
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 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, 0.1 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 CROCUBE
1 62394U 24247T   26221.71842102  .00030956  00000-0  50351-3 0  9991
2 62394  44.9718 317.0013 0009752 323.3706  36.6518 15.52128692 91652
Epoch: 2026-08-09T17:14Z
TLE epoch observation values (Epoch: 2026-08-09T17:14:31.576Z)
Latitude
-0.00004°
Longitude
100.15831°
Altitude
405.199 km
Speed
7.672 km/s
True Right ascension
21h 08m 00s
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
22:54:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
418.765 km
Perigee altitude
405.521 km
Semi-major axis
6,790.28 km
Eccentricity
0.00098
Inclination
44.9718°
RAAN
317.0013°
Arg. of periapsis
323.3706°
True anomaly
36.71857°
Mean anomaly
36.6518°
Eccentric anomaly
36.68518°
Mean motion
3.87893 °/min
Orbital period
92.81 mins
BSTAR
0.00050351
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