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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: 8 hours ago

TLE from 8 hours ago
0 FUNCUBE 1
1 39444U 13066AE  26037.84419360  .00012699  00000-0  83269-3 0  9991
2 39444  97.8149   6.8858 0035867 288.2356  71.4968 15.07294695660018
Epoch: 2026-02-06T20:15Z
TLE epoch observation values (Epoch: 2026-02-06T20:15:38.327Z)
Latitude
-0.00007°
Longitude
-74.00013°
Altitude
539.731 km
Speed
7.597 km/s
True Right ascension
00h 27m 32s
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
06:00:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
566.29 km
Perigee altitude
516.653 km
Semi-major axis
6,919.608 km
Eccentricity
0.00359
Inclination
97.8149°
RAAN
6.8858°
Arg. of periapsis
288.2356°
True anomaly
71.88711°
Mean anomaly
71.4968°
Eccentric anomaly
71.6919°
Mean motion
3.77069 °/min
Orbital period
95.47 mins
BSTAR
0.00083269
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