DECAYED
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W-CUBE, 48965 (Decayed)

Orbit data source: Space-Track

W-CUBE, 48965 was a payload satellite owned by Reaktor Space (FI) in LEO that was launched on Wed, 30 Jun 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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.

Not visible in the next 10 days
Identifier
48965, 2021-059CQ
Orbit
Decayed
Country
Flag of FIFI / FIN
Related business
Manufacturer
Reaktor Space
Mission
Decayed Commercial Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
2021-06-30 (4 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

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

TLE from 1 month ago
0 W-CUBE
1 48965U 21059CQ  25273.10988651  .03797464  26509-5  82303-3 0  9992
2 48965  97.6531  97.9098 0006615 262.0715  97.9828 16.30605806237996
Epoch: 2025-09-30T02:38Z
TLE epoch observation values (Epoch: 2025-09-30T02:38:14.194Z)
Latitude
-0.00002°
Longitude
49.2467°
Altitude
194.75 km
Speed
7.789 km/s
True Right ascension
06h 31m 38s
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
16:31:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
192.087 km
Perigee altitude
183.4 km
Semi-major axis
6,565.881 km
Eccentricity
0.00066
Inclination
97.6531°
RAAN
97.9098°
Arg. of periapsis
262.0715°
True anomaly
98.05786°
Mean anomaly
97.9828°
Eccentric anomaly
98.02033°
Mean motion
4.07947 °/min
Orbital period
88.25 mins
BSTAR
0.00082303
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Computing Atmospheric mass density...

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