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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.

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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: 23 hours ago

TLE from 23 hours ago
0 QB50P2
1 40032U 14033Y   25338.40637354  .00019321  00000-0  11388-2 0  9992
2 40032  98.0629 318.8104 0009726 111.9216 248.3047 15.11593495623209
Epoch: 2025-12-04T09:45Z
TLE epoch observation values (Epoch: 2025-12-04T09:45:10.673Z)
Latitude
-0.00009°
Longitude
99.05267°
Altitude
536.89 km
Speed
7.593 km/s
True Right ascension
21h 15m 14s
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
06:38:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
535.063 km
Perigee altitude
521.629 km
Semi-major axis
6,906.483 km
Eccentricity
0.00097
Inclination
98.0629°
RAAN
318.8104°
Arg. of periapsis
111.9216°
True anomaly
248.20119°
Mean anomaly
248.3047°
Eccentric anomaly
248.25294°
Mean motion
3.78144 °/min
Orbital period
95.2 mins
BSTAR
0.0011388
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