UNICORN-2S, 68475
Orbit data source: Space-Track
UNICORN-2S, 68475 is a payload satellite owned by Alba Orbital (DE) in SSO that was launched on Mon, 30 Mar 2026 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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68475 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 UNICORN-2S
1 68475U 26067BM 26217.41253553 .00006048 00000-0 58958-3 0 9993
2 68475 97.7523 174.7908 0001818 239.7507 120.3533 14.92825024 18544Epoch: 2026-08-05T09:54Z
TLE epoch observation values (Epoch: 2026-08-05T09:54:03.069Z)
Latitude
0°
Longitude
72.31071°
Altitude
592.816 km
Speed
7.563 km/s
True Right ascension
11h 39m 09s
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
23:15:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.415 km
Perigee altitude
584.883 km
Semi-major axis
6,964.286 km
Eccentricity
0.00018
Inclination
97.7523°
RAAN
174.7908°
Arg. of periapsis
239.7507°
True anomaly
120.37128°
Mean anomaly
120.3533°
Eccentric anomaly
120.36229°
Mean motion
3.73446 °/min
Orbital period
96.4 mins
BSTAR
0.00058958
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Other satellites on launch #67 in the year 2026 (2026-03-30 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-2S 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-06 10:35:57.320Z | 351.322° N | 2026-08-06 10:38:57.320Z | 284.844° WNW | 32.839° | 2026-08-06 10:41:57.320Z | 222.877° SW |
| 7 mins | 2026-08-06 21:24:57.320Z | 177.38° S | 2026-08-06 21:27:57.320Z | 235.667° WSW | 42.376° | 2026-08-06 21:31:57.320Z | 341.501° 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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