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: 17 hours ago
TLE from 17 hours ago
0 UNICORN-2R
1 68477U 26067BP 26263.13664404 .00005894 00000-0 57105-3 0 9997
2 68477 97.7586 219.8448 0006048 104.5499 255.6392 14.93071976 25299Epoch: 2026-09-20T03:16Z
TLE epoch observation values (Epoch: 2026-09-20T03:16:46.045Z)
Latitude
0.00004°
Longitude
171.61779°
Altitude
592.455 km
Speed
7.563 km/s
True Right ascension
14h 39m 22s
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
12:54:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.592 km
Perigee altitude
581.169 km
Semi-major axis
6,963.518 km
Eccentricity
0.0006
Inclination
97.7586°
RAAN
219.8448°
Arg. of periapsis
104.5499°
True anomaly
255.57207°
Mean anomaly
255.6392°
Eccentric anomaly
255.60564°
Mean motion
3.73508 °/min
Orbital period
96.38 mins
BSTAR
0.00057105
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-20 21:05:55.168Z | 157.882° S | 2026-09-20 21:08:55.168Z | 107.672° ESE | 68.64° | 2026-09-20 21:12:55.168Z | 352.675° N |
| 6 mins | 2026-09-21 10:24:55.168Z | 356.782° N | 2026-09-21 10:27:55.168Z | 261.697° W | 52.28° | 2026-09-21 10:30:55.168Z | 210.692° SW |
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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