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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 (1 year 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, Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 CROCUBE
1 62394U 24247T   26036.99781542  .00044088  00000-0  11195-2 0  9998
2 62394  44.9735 273.7889 0002212 191.4907 168.5929 15.39013829 63077
Epoch: 2026-02-05T23:56Z
TLE epoch observation values (Epoch: 2026-02-05T23:56:51.252Z)
Latitude
-0.00007°
Longitude
138.43327°
Altitude
450.5 km
Speed
7.643 km/s
True Right ascension
18h 15m 09s
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
10:00:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
452.156 km
Perigee altitude
449.135 km
Semi-major axis
6,828.783 km
Eccentricity
0.00022
Inclination
44.9735°
RAAN
273.7889°
Arg. of periapsis
191.4907°
True anomaly
168.59791°
Mean anomaly
168.5929°
Eccentric anomaly
168.59541°
Mean motion
3.84617 °/min
Orbital period
93.6 mins
BSTAR
0.0011195
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Documentation

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