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 Amateur Earth Obs Sci
Bus & Motor
CUBESAT 2U, Unknown motor
Mass
~2 kg wet, ~2 kg dry
Launch date (UTC)
2014-06-19 (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
0.025 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 QB50P2
1 40032U 14033Y   26297.27886302  .00005572  00000-0  28866-3 0  9994
2 40032  98.0805 302.3947 0009007  94.6394 265.5866 15.16616344672224
Epoch: 2026-10-24T06:41Z
TLE epoch observation values (Epoch: 2026-10-24T06:41:33.764Z)
Latitude
-0.00008°
Longitude
169.31669°
Altitude
519.625 km
Speed
7.603 km/s
True Right ascension
20h 09m 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
16:35:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
519.283 km
Perigee altitude
506.869 km
Semi-major axis
6,891.213 km
Eccentricity
0.0009
Inclination
98.0805°
RAAN
302.3947°
Arg. of periapsis
94.6394°
True anomaly
265.4837°
Mean anomaly
265.5866°
Eccentric anomaly
265.53515°
Mean motion
3.79402 °/min
Orbital period
94.89 mins
BSTAR
0.00028866
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
|