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QB50P1, 40025

Orbit data source: Space-Track

QB50P1, 40025 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
40025, 2014-033R
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, Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 QB50P1
1 40025U 14033R   26171.31353525  .00007093  00000-0  34929-3 0  9995
2 40025  98.0964 182.6784 0008083 203.9686 156.1171 15.18299167653508
Epoch: 2026-06-20T07:31Z
TLE epoch observation values (Epoch: 2026-06-20T07:31:29.445Z)
Latitude
-0.00003°
Longitude
161.27577°
Altitude
519.142 km
Speed
7.601 km/s
True Right ascension
12h 10m 42s
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
21:43:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.546 km
Perigee altitude
502.414 km
Semi-major axis
6,886.117 km
Eccentricity
0.00081
Inclination
98.0964°
RAAN
182.6784°
Arg. of periapsis
203.9686°
True anomaly
156.15457°
Mean anomaly
156.1171°
Eccentric anomaly
156.13584°
Mean motion
3.79823 °/min
Orbital period
94.78 mins
BSTAR
0.00034929
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