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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Edit Public Description
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: 23 hours ago
TLE from 23 hours ago
0 UNICORN-2P
1 63981U 25052BT 25298.21574326 .00067940 00000-0 22257-2 0 9993
2 63981 97.4112 190.2467 0005776 99.3637 260.8258 15.31382646 34179Epoch: 2025-10-25T05:10Z
TLE epoch observation values (Epoch: 2025-10-25T05:10:40.217Z)
Latitude
0.00001°
Longitude
78.72964°
Altitude
475.425 km
Speed
7.628 km/s
True Right ascension
12h 40m 59s
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
23:10:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
472.592 km
Perigee altitude
464.682 km
Semi-major axis
6,846.774 km
Eccentricity
0.00058
Inclination
97.4112°
RAAN
190.2467°
Arg. of periapsis
99.3637°
True anomaly
260.76047°
Mean anomaly
260.8258°
Eccentric anomaly
260.79313°
Mean motion
3.83102 °/min
Orbital period
93.97 mins
BSTAR
0.0022257
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-26 05:16:05.442Z | 37.804° NE | 2025-10-26 05:19:05.442Z | 110.066° ESE | 26.323° | 2025-10-26 05:21:05.442Z | 153.882° SSE |
| 5 mins | 2025-10-26 17:23:05.442Z | 202.934° SW | 2025-10-26 17:25:05.442Z | 267.816° W | 32.495° | 2025-10-26 17:28:05.442Z | 331.598° NNW |
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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