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FUNCUBE 1, 39444

Orbit data source: Space-Track

FUNCUBE 1, 39444 is a UK payload satellite in SSO that was launched on Thu, 21 Nov 2013 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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
39444, 2013-066AE
Orbit
SSO
Country
Flag of UKUK
Related business
Manufacturer
ISIS BV
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
2013-11-21 (12 years ago)
Launch vehicle
DNEPR
Launch site
Orenburg, Russia (OREN)
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: 1 day ago

TLE from 1 day ago
0 FUNCUBE 1
1 39444U 13066AE  26091.66443671  .00011179  00000-0  71133-3 0  9992
2 39444  97.8217  61.6044 0038870 103.4180 257.1385 15.08333682668127
Epoch: 2026-04-01T15:56Z
TLE epoch observation values (Epoch: 2026-04-01T15:56:47.331Z)
Latitude
-0.00001°
Longitude
-7.61683°
Altitude
550.441 km
Speed
7.583 km/s
True Right ascension
04h 06m 25s
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
01:16:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
565.175 km
Perigee altitude
511.407 km
Semi-major axis
6,916.428 km
Eccentricity
0.00389
Inclination
97.8217°
RAAN
61.6044°
Arg. of periapsis
103.418°
True anomaly
256.70473°
Mean anomaly
257.1385°
Eccentric anomaly
256.92157°
Mean motion
3.77329 °/min
Orbital period
95.41 mins
BSTAR
0.00071133
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