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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Identifier
Orbit
Country
BE / BELRelated business
Manufacturer
ISIS BV
Mission
Operational Amateur Earth Obs Sci
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
0.025 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 QB50P1
1 40025U 14033R 26251.29185855 .00006800 00000-0 32487-3 0 9992
2 40025 98.0975 268.3424 0007070 307.8140 52.2452 15.19376732665648Epoch: 2026-09-08T07:00Z
TLE epoch observation values (Epoch: 2026-09-08T07:00:16.578Z)
Latitude
-0.00006°
Longitude
175.91296°
Altitude
507.813 km
Speed
7.612 km/s
True Right ascension
17h 53m 22s
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
06:40:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.587 km
Perigee altitude
499.854 km
Semi-major axis
6,882.858 km
Eccentricity
0.00071
Inclination
98.0975°
RAAN
268.3424°
Arg. of periapsis
307.814°
True anomaly
52.30929°
Mean anomaly
52.2452°
Eccentric anomaly
52.27724°
Mean motion
3.80093 °/min
Orbital period
94.71 mins
BSTAR
0.00032487
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-09 00:33:11.802Z | 105.087° ESE | 2026-09-09 00:34:11.802Z | 82.522° E | 24.365° | 2026-09-09 00:37:11.802Z | 19.041° NNE |
| 4 mins | 2026-09-09 02:07:11.802Z | 238.034° WSW | 2026-09-09 02:08:11.802Z | 258.793° W | 19.447° | 2026-09-09 02:11:11.802Z | 312.554° NW |
| 5 mins | 2026-09-09 13:37:11.802Z | 46.424° ENE | 2026-09-09 13:39:11.802Z | 96.844° ESE | 32.456° | 2026-09-09 13:42:11.802Z | 160.114° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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