Showing default

CUBEBUG 2, 39440

Orbit data source: Space-Track

CUBEBUG 2, 39440 is a payload satellite owned by MinCyT (AR) 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.

Loading next visibility...
Identifier
39440, 2013-066AA
Orbit
SSO
Country
Flag of UnknownUnknown / ARGN
Related business
Manufacturer
INVAP
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 2U, Unknown motor
Mass
3 kg wet, 3 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, 1.0 m
Radar Cross Section
0.040 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 CUBEBUG 2
1 39440U 13066AA  26037.79615627  .00006647  00000-0  62887-3 0  9994
2 39440  97.8775 346.4411 0060814  99.2482 261.5622 14.92581267657536
Epoch: 2026-02-06T19:06Z
TLE epoch observation values (Epoch: 2026-02-06T19:06:27.901Z)
Latitude
-0.00001°
Longitude
-77.10405°
Altitude
599.401 km
Speed
7.556 km/s
True Right ascension
23h 05m 45s
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
04:20:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
629.271 km
Perigee altitude
544.556 km
Semi-major axis
6,965.05 km
Eccentricity
0.00608
Inclination
97.8775°
RAAN
346.4411°
Arg. of periapsis
99.2482°
True anomaly
260.87365°
Mean anomaly
261.5622°
Eccentric anomaly
261.21785°
Mean motion
3.73385 °/min
Orbital period
96.42 mins
BSTAR
0.00062887
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|