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 spacecraft
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
Unknown shape, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 UNICORN-2S
1 68475U 26067BM 26171.41951062 .00007294 00000-0 72319-3 0 9993
2 68475 97.7504 129.5084 0005921 60.0512 300.1294 14.92071727 11689Epoch: 2026-06-20T10:04Z
TLE epoch observation values (Epoch: 2026-06-20T10:04:05.717Z)
Latitude
-0.00005°
Longitude
69.85018°
Altitude
592.449 km
Speed
7.565 km/s
True Right ascension
08h 38m 02s
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
15:44:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.62 km
Perigee altitude
584.37 km
Semi-major axis
6,966.632 km
Eccentricity
0.00059
Inclination
97.7504°
RAAN
129.5084°
Arg. of periapsis
60.0512°
True anomaly
300.0707°
Mean anomaly
300.1294°
Eccentric anomaly
300.10005°
Mean motion
3.73258 °/min
Orbital period
96.45 mins
BSTAR
0.00072319
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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 | 2026-06-22 09:19:31.952Z | 45.059° ENE | 2026-06-22 09:22:31.952Z | 99.144° ESE | 22.575° | 2026-06-22 09:25:31.952Z | 148.886° SSE |
| 5 mins | 2026-06-22 10:55:31.952Z | 335.217° NNW | 2026-06-22 10:57:31.952Z | 298.177° NW | 22.905° | 2026-06-22 11:00:31.952Z | 241.827° WSW |
| 5 mins | 2026-06-22 21:45:31.952Z | 206.849° SW | 2026-06-22 21:47:31.952Z | 257.932° W | 32.08° | 2026-06-22 21:50:31.952Z | 325.038° 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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