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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40025 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: 8 hours ago
TLE from 8 hours ago
0 QB50P1
1 40025U 14033R 25343.51436768 .00013111 00000-0 71734-3 0 9991
2 40025 98.0971 336.9048 0010291 144.1390 216.0533 15.14357306624282Epoch: 2025-12-09T12:20Z
TLE epoch observation values (Epoch: 2025-12-09T12:20:41.367Z)
Latitude
-0°
Longitude
73.23448°
Altitude
531.738 km
Speed
7.594 km/s
True Right ascension
22h 27m 37s
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
18:24:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
527.033 km
Perigee altitude
512.836 km
Semi-major axis
6,898.072 km
Eccentricity
0.00103
Inclination
98.0971°
RAAN
336.9048°
Arg. of periapsis
144.139°
True anomaly
215.98397°
Mean anomaly
216.0533°
Eccentric anomaly
216.01863°
Mean motion
3.78836 °/min
Orbital period
95.03 mins
BSTAR
0.00071734
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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.QB50P1 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-09 23:33:55.581Z | 157.301° SSE | 2025-12-09 23:37:55.581Z | 33.084° NE | 41.146° | 2025-12-09 23:40:55.581Z | 353.307° N |
| 5 mins | 2025-12-10 12:42:55.581Z | 8.857° NNE | 2025-12-10 12:44:55.581Z | 230.599° WSW | 44.303° | 2025-12-10 12:47:55.581Z | 196.975° SSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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