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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40032 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
BE / BELRelated business
Manufacturer
ISIS BV
Mission
Operational Civil Science
Bus & Motor
CUBESAT 2U, Unknown motor
Mass
~2 kg wet, ~2 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.040 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 QB50P2
1 40032U 14033Y 25285.69220729 .00012998 00000-0 79547-3 0 9993
2 40032 98.0582 263.2903 0006386 307.7916 52.2733 15.10347467615242Epoch: 2025-10-12T16:36Z
TLE epoch observation values (Epoch: 2025-10-12T16:36:46.709Z)
Latitude
-0.00006°
Longitude
-7.41001°
Altitude
535.497 km
Speed
7.596 km/s
True Right ascension
17h 33m 09s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
11:10:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
536.56 km
Perigee altitude
527.734 km
Semi-major axis
6,910.284 km
Eccentricity
0.00064
Inclination
98.0582°
RAAN
263.2903°
Arg. of periapsis
307.7916°
True anomaly
52.33121°
Mean anomaly
52.2733°
Eccentric anomaly
52.30225°
Mean motion
3.77832 °/min
Orbital period
95.28 mins
BSTAR
0.00079547
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Other satellites on launch #33 in the year 2014 (2014-06-19 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.QB50P2 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-13 22:57:36.085Z | 191.943° SSW | 2025-10-13 22:59:36.085Z | 244.341° WSW | 37.089° | 2025-10-13 23:02:36.085Z | 331.192° NNW |
| 4 mins | 2025-10-14 12:07:36.085Z | 330.776° NNW | 2025-10-14 12:08:36.085Z | 305.32° NW | 27.851° | 2025-10-14 12:11:36.085Z | 232.277° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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