Showing default

QB50P2, 40032

Orbit data source: Space-Track

QB50P2, 40032 is a payload satellite owned by QB50 (BE) in SSO that was launched on Thu, 19 Jun 2014 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
40032, 2014-033Y
Orbit
SSO
Country
Flag of BEBE / BEL
Related business
Manufacturer
ISIS BV
Mission
Operational Civil Science
Bus & Motor
CUBESAT 2U, Unknown motor
Mass
~2 kg wet, ~2 kg dry
Launch date (UTC)
2014-06-19 (11 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
0.040 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 QB50P2
1 40032U 14033Y   25334.69922444  .00009874  00000-0  58648-3 0  9999
2 40032  98.0632 314.9022 0009282 122.5821 237.6305 15.11493912622644
Epoch: 2025-11-30T16:46Z
TLE epoch observation values (Epoch: 2025-11-30T16:46:52.991Z)
Latitude
-0.00003°
Longitude
-6.62792°
Altitude
538.141 km
Speed
7.592 km/s
True Right ascension
20h 59m 36s
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
23:27:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
535.061 km
Perigee altitude
522.239 km
Semi-major axis
6,906.787 km
Eccentricity
0.00093
Inclination
98.0632°
RAAN
314.9022°
Arg. of periapsis
122.5821°
True anomaly
237.54072°
Mean anomaly
237.6305°
Eccentric anomaly
237.5856°
Mean motion
3.7812 °/min
Orbital period
95.21 mins
BSTAR
0.00058648
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
|