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: 22 hours ago
TLE from 22 hours ago
0 UNICORN-2S
1 68475U 26067BM 26264.12229025 .00005060 00000-0 48666-3 0 9998
2 68475 97.7593 220.8523 0005875 89.2125 270.9768 14.93432454 25517Epoch: 2026-09-21T02:56Z
TLE epoch observation values (Epoch: 2026-09-21T02:56:05.877Z)
Latitude
-0.00001°
Longitude
176.82116°
Altitude
590.219 km
Speed
7.565 km/s
True Right ascension
14h 43m 24s
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
18:19:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.35 km
Perigee altitude
580.169 km
Semi-major axis
6,962.396 km
Eccentricity
0.00059
Inclination
97.7593°
RAAN
220.8523°
Arg. of periapsis
89.2125°
True anomaly
270.90949°
Mean anomaly
270.9768°
Eccentric anomaly
270.94314°
Mean motion
3.73598 °/min
Orbital period
96.36 mins
BSTAR
0.00048666
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-22 10:03:12.056Z | 14.517° NNE | 2026-09-22 10:06:12.056Z | 31.741° NE | 69.031° | 2026-09-22 10:10:12.056Z | 190.411° SSW |
| 6 mins | 2026-09-22 20:53:12.056Z | 139.13° SSE | 2026-09-22 20:55:12.056Z | 95.868° ESE | 46.044° | 2026-09-22 20:59:12.056Z | 1.041° NNE |
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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