Showing default

UNICORN-2M, 58726

Orbit data source: Space-Track

UNICORN-2M, 58726 is 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.

Loading next visibility...
Identifier
58726, 2023-185Q
Orbit
SSO
Country
Flag of DEDE / GER
Related 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)
2023-12-01 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.016 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 UNICORN-2M
1 58726U 23185Q   25306.50363383  .00068141  00000-0  12487-2 0  9998
2 58726  97.5692  26.6398 0005133 339.6932  20.4114 15.49062207101223
Epoch: 2025-11-02T12:05Z
TLE epoch observation values (Epoch: 2025-11-02T12:05:13.962Z)
Latitude
Longitude
163.3132°
Altitude
419.322 km
Speed
7.661 km/s
True Right ascension
01h 46m 33s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
23:56:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
419.89 km
Perigee altitude
412.915 km
Semi-major axis
6,794.54 km
Eccentricity
0.00051
Inclination
97.5692°
RAAN
26.6398°
Arg. of periapsis
339.6932°
True anomaly
20.43193°
Mean anomaly
20.4114°
Eccentric anomaly
20.42166°
Mean motion
3.87528 °/min
Orbital period
92.9 mins
BSTAR
0.0012487
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|