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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 (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
0.040 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 QB50P2
1 40032U 14033Y   26123.97597405  .00007595  00000-0  41514-3 0  9994
2 40032  98.0756 118.1274 0006591 339.8250  20.2719 15.14594410645977
Epoch: 2026-05-03T23:25Z
TLE epoch observation values (Epoch: 2026-05-03T23:25:24.157Z)
Latitude
-0.00003°
Longitude
-95.09505°
Altitude
521.006 km
Speed
7.605 km/s
True Right ascension
07h 52m 30s
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
20:12:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
523.759 km
Perigee altitude
514.667 km
Semi-major axis
6,897.35 km
Eccentricity
0.00066
Inclination
98.0756°
RAAN
118.1274°
Arg. of periapsis
339.825°
True anomaly
20.29809°
Mean anomaly
20.2719°
Eccentric anomaly
20.28499°
Mean motion
3.78896 °/min
Orbital period
95.01 mins
BSTAR
0.00041514
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