UNICORN-2P, 63981 (Decayed)
Orbit data source: Space-Track
UNICORN-2P, 63981 was a payload satellite owned by Alba Orbital (DE) in LEO that was launched on Sat, 15 Mar 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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63981 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
Alba Orbital
Mission
Decayed Commercial Imaging
Bus & Motor
POCKETQUBE 3P, Unknown motor
Mass
~0.75 kg wet, ~0.75 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.016 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 UNICORN-2P
1 63981U 25052BT 26061.66207681 .09079400 24721-5 43819-2 0 9999
2 63981 97.3656 322.3272 0007474 166.9554 193.1930 16.21219791 54086Epoch: 2026-03-02T15:53Z
TLE epoch observation values (Epoch: 2026-03-02T15:53:23.436Z)
Latitude
-0.00005°
Longitude
-76.47272°
Altitude
224.269 km
Speed
7.769 km/s
True Right ascension
21h 29m 18s
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
23:12:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
217.999 km
Perigee altitude
208.146 km
Semi-major axis
6,591.21 km
Eccentricity
0.00075
Inclination
97.3656°
RAAN
322.3272°
Arg. of periapsis
166.9554°
True anomaly
193.17347°
Mean anomaly
193.193°
Eccentric anomaly
193.18323°
Mean motion
4.05598 °/min
Orbital period
88.76 mins
BSTAR
0.0043819
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Other satellites on launch #52 in the year 2025 (2025-03-15 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.UNICORN-2P Visibility
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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. |
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| This satellite is decayed. |
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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