Showing default

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.

Loading next visibility...
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, Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 QB50P1
1 40025U 14033R   26033.46620448  .00010330  00000-0  54555-3 0  9994
2 40025  98.0988  35.3980 0008257 339.6183  20.4717 15.15699912632604
Epoch: 2026-02-02T11:11Z
TLE epoch observation values (Epoch: 2026-02-02T11:11:20.067Z)
Latitude
-0°
Longitude
94.9033°
Altitude
516.583 km
Speed
7.608 km/s
True Right ascension
02h 21m 35s
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
23:50:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
521.549 km
Perigee altitude
510.165 km
Semi-major axis
6,893.994 km
Eccentricity
0.00083
Inclination
98.0988°
RAAN
35.398°
Arg. of periapsis
339.6183°
True anomaly
20.50482°
Mean anomaly
20.4717°
Eccentric anomaly
20.48826°
Mean motion
3.79172 °/min
Orbital period
94.94 mins
BSTAR
0.00054555
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
|