UNICORN-2R, 68477
Orbit data source: Space-Track
UNICORN-2R, 68477 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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68477 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: 1 day ago
TLE from 1 day ago
0 UNICORN-2R
1 68477U 26067BP 26259.11553585 .00008000 00000-0 77381-3 0 9997
2 68477 97.7595 215.8784 0006142 112.5988 247.5882 14.93025116 24697Epoch: 2026-09-16T02:46Z
TLE epoch observation values (Epoch: 2026-09-16T02:46:22.297Z)
Latitude
0°
Longitude
179.21374°
Altitude
593.187 km
Speed
7.562 km/s
True Right ascension
14h 23m 30s
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
07:17:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.804 km
Perigee altitude
581.249 km
Semi-major axis
6,963.664 km
Eccentricity
0.00061
Inclination
97.7595°
RAAN
215.8784°
Arg. of periapsis
112.5988°
True anomaly
247.52315°
Mean anomaly
247.5882°
Eccentric anomaly
247.55567°
Mean motion
3.73496 °/min
Orbital period
96.39 mins
BSTAR
0.00077381
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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-2R 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 | 2026-09-17 20:43:50.533Z | 134.132° SE | 2026-09-17 20:46:50.533Z | 68.495° E | 38.293° | 2026-09-17 20:49:50.533Z | 8.541° NNE |
| 4 mins | 2026-09-17 22:20:50.533Z | 241.952° WSW | 2026-09-17 22:22:50.533Z | 275.469° WNW | 15.816° | 2026-09-17 22:24:50.533Z | 304.793° NW |
| 6 mins | 2026-09-18 10:02:50.533Z | 17.901° NNE | 2026-09-18 10:04:50.533Z | 59.773° ENE | 76.053° | 2026-09-18 10:08:50.533Z | 189.31° SSW |
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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