UNICORN-2O, 63980
Orbit data source: Space-Track
UNICORN-2O, 63980 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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63980 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, 0.1 m
Radar Cross Section
0.016 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 UNICORN-2O
1 63980U 25052BS 25299.64759686 .00078168 00000-0 25290-2 0 9998
2 63980 97.4105 191.6995 0005928 100.3029 259.8881 15.31735932 34392Epoch: 2025-10-26T15:32Z
TLE epoch observation values (Epoch: 2025-10-26T15:32:32.368Z)
Latitude
-0.00004°
Longitude
-76.69615°
Altitude
474.454 km
Speed
7.628 km/s
True Right ascension
12h 46m 47s
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
20:01:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.641 km
Perigee altitude
463.525 km
Semi-major axis
6,845.72 km
Eccentricity
0.00059
Inclination
97.4105°
RAAN
191.6995°
Arg. of periapsis
100.3029°
True anomaly
259.82123°
Mean anomaly
259.8881°
Eccentric anomaly
259.85467°
Mean motion
3.8319 °/min
Orbital period
93.95 mins
BSTAR
0.002529
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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-2O 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 | 2025-10-27 06:13:08.274Z | 347.74° N | 2025-10-27 06:15:08.274Z | 293.998° NW | 32.342° | 2025-10-27 06:18:08.274Z | 218.839° SW |
| 5 mins | 2025-10-27 16:46:08.274Z | 148.495° SSE | 2025-10-27 16:48:08.274Z | 86.279° E | 39.977° | 2025-10-27 16:51:08.274Z | 358.275° 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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