UNICORN-2P, 63981
Orbit data source: Space-Track
UNICORN-2P, 63981 is a payload satellite owned by Alba Orbital (DE) in SSO 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
Operational 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: 7 hours ago
TLE from 7 hours ago
0 UNICORN-2P
1 63981U 25052BT 26055.21098159 .01014694 00000-0 35713-2 0 9990
2 63981 97.3835 315.2410 0007872 104.9147 255.2996 15.86748854 53057Epoch: 2026-02-24T05:03Z
TLE epoch observation values (Epoch: 2026-02-24T05:03:48.809Z)
Latitude
-0.00005°
Longitude
85.19387°
Altitude
315.926 km
Speed
7.718 km/s
True Right ascension
21h 00m 57s
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
15:16:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
313.545 km
Perigee altitude
303.018 km
Semi-major axis
6,686.418 km
Eccentricity
0.00079
Inclination
97.3835°
RAAN
315.241°
Arg. of periapsis
104.9147°
True anomaly
255.21237°
Mean anomaly
255.2996°
Eccentric anomaly
255.25598°
Mean motion
3.96966 °/min
Orbital period
90.69 mins
BSTAR
0.0035713
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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 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 | 2026-02-24 17:17:59.138Z | 167.064° S | 2026-02-24 17:19:59.138Z | 165.578° S | 43.015° | 2026-02-24 17:21:59.138Z | 348.209° N |
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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