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FUNCUBE 1, 39444

Orbit data source: Space-Track

FUNCUBE 1, 39444 is a 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
Last TLE update
6 hours ago
Origin
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

TLE from 6 hours ago
0 FUNCUBE 1
1 39444U 13066AE  25149.15701127  .00008002  00000-0  59992-3 0  9992
2 39444  97.7841 111.0277 0044272  66.7599 293.8278 15.02150735622460
Epoch: 2025-05-29T03:46Z
TLE epoch observation values (Epoch: 2025-05-29T03:46:05.773Z)
Latitude
-0.00001°
Longitude
167.57351°
Altitude
551.023 km
Speed
7.593 km/s
True Right ascension
07h 24m 06s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
22.96397°
Longitude
164.54271°
Altitude
540.511 km
Speed
7.607 km/s
Apparent Right ascension
07h 25m 59s
Apparent Declination
-7° 01' 53"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
19:44:12
Azimuth
8.291° NNE
Elevation
-56.862°
Doppler factor
1
Orbital elements
Apogee altitude
587.976 km
Perigee altitude
526.567 km
Semi-major axis
6,935.409 km
Eccentricity
0.00443
Inclination
97.7841°
RAAN
111.0277°
Arg. of periapsis
66.7599°
True anomaly
Unknown
Mean anomaly
293.8278°
Eccentric anomaly
Unknown
Mean motion
3.75781 °/min
Orbital period
95.8 mins
BSTAR
0.00059992
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FUNCUBE 1 Visibility forecast

Observer location: undefined°, undefined°

Span
Click to sort rows by Start time (UTC) header in descending order
Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
7 mins2025-05-29 10:42:53.602Z358.345° N2025-05-29 10:46:53.602Z263.534° W34.088°2025-05-29 10:49:53.602Z215.145° SW
5 mins2025-05-29 21:29:53.602Z168.544° S2025-05-29 21:31:53.602Z273.175° WNW44.962°2025-05-29 21:34:53.602Z346.631° N
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