UNICORN-2M, 58726 (Decayed)
Orbit data source: Space-Track
UNICORN-2M, 58726 was a payload satellite owned by Alba Orbital (DE) in SSO that was launched on Fri, 01 Dec 2023 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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58726 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
Alba Orbital
Mission
Decayed 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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 UNICORN-2M
1 58726U 23185Q 26047.73080617 .00634840 00000-0 31271-2 0 9999
2 58726 97.5498 139.9015 0006986 286.3482 73.7016 15.80469206117792Epoch: 2026-02-16T17:32Z
TLE epoch observation values (Epoch: 2026-02-16T17:32:21.653Z)
Latitude
-0.00008°
Longitude
90.09034°
Altitude
330.968 km
Speed
7.711 km/s
True Right ascension
09h 19m 36s
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
20:16:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
330.688 km
Perigee altitude
321.321 km
Semi-major axis
6,704.142 km
Eccentricity
0.0007
Inclination
97.5498°
RAAN
139.9015°
Arg. of periapsis
286.3482°
True anomaly
73.77846°
Mean anomaly
73.7016°
Eccentric anomaly
73.74003°
Mean motion
3.95392 °/min
Orbital period
91.05 mins
BSTAR
0.0031271
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Other satellites on launch #185 in the year 2023 (2023-12-01 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-2M Visibility
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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