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ZACUBE, 39417

Orbit data source: Space-Track

ZACUBE, 39417 is a payload satellite owned by CPUT (ZA) 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
39417, 2013-066B
Orbit
SSO
Country
Flag of ZAZA / SAFR
Related business
Manufacturer
CPUT
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1.2 kg wet, 1.2 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: 11 hours ago

TLE from 11 hours ago
0 ZACUBE
1 39417U 13066B   26092.20470413  .00005155  00000-0  40496-3 0  9992
2 39417  97.8143  54.1428 0044878 143.5169 216.9127 15.00546651669330
Epoch: 2026-04-02T04:54Z
TLE epoch observation values (Epoch: 2026-04-02T04:54:46.436Z)
Latitude
-0.00002°
Longitude
149.89278°
Altitude
593.232 km
Speed
7.55 km/s
True Right ascension
03h 36m 34s
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
21:48:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.366 km
Perigee altitude
531.072 km
Semi-major axis
6,940.356 km
Eccentricity
0.00449
Inclination
97.8143°
RAAN
54.1428°
Arg. of periapsis
143.5169°
True anomaly
216.60522°
Mean anomaly
216.9127°
Eccentric anomaly
216.75882°
Mean motion
3.75379 °/min
Orbital period
95.9 mins
BSTAR
0.00040496
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