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: 17 hours ago
TLE from 17 hours ago
0 UNICORN-2O
1 63980U 25052BS 25345.21453091 .00192696 00000-0 41703-2 0 9994
2 63980 97.4070 237.6435 0005993 53.2447 306.9350 15.43709991 41397Epoch: 2025-12-11T05:08Z
TLE epoch observation values (Epoch: 2025-12-11T05:08:55.470Z)
Latitude
-0.00007°
Longitude
80.23867°
Altitude
435.841 km
Speed
7.652 km/s
True Right ascension
15h 50m 34s
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
20:03:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
436.187 km
Perigee altitude
428.024 km
Semi-major axis
6,810.242 km
Eccentricity
0.0006
Inclination
97.407°
RAAN
237.6435°
Arg. of periapsis
53.2447°
True anomaly
306.88008°
Mean anomaly
306.935°
Eccentric anomaly
306.90754°
Mean motion
3.86188 °/min
Orbital period
93.22 mins
BSTAR
0.0041703
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-12 05:03:23.683Z | 54.683° ENE | 2025-12-12 05:05:23.683Z | 94.19° ESE | 16.122° | 2025-12-12 05:07:23.683Z | 134° SE |
| 4 mins | 2025-12-12 17:04:23.683Z | 167.722° S | 2025-12-12 17:05:23.683Z | 168.729° S | 42.278° | 2025-12-12 17:08:23.683Z | 347.825° 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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