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SONATE-2, 59112

Orbit data source: Space-Track

SONATE-2, 59112 is a payload satellite owned by U Wurzburg (DE) in SSO that was launched on Mon, 04 Mar 2024 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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Identifier
59112, 2024-043Q
Orbit
SSO
Country
Flag of DEDE / GER
Related business
Manufacturer
U Wurzburg
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~12 kg wet, ~12 kg dry
Launch date (UTC)
2024-03-04 (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, 0.3 m
Radar Cross Section
0.051 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 SONATE-2
1 59112U 24043Q   25297.63491000  .00031323  00000-0  74250-3 0  9992
2 59112  97.5309  72.1982 0009449 346.4139  13.6852 15.41645351 91402
Epoch: 2025-10-24T15:14Z
TLE epoch observation values (Epoch: 2025-10-24T15:14:16.224Z)
Latitude
0.00004°
Longitude
170.35361°
Altitude
438.107 km
Speed
7.652 km/s
True Right ascension
04h 48m 47s
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
20:15:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
444.636 km
Perigee altitude
431.755 km
Semi-major axis
6,816.332 km
Eccentricity
0.00094
Inclination
97.5309°
RAAN
72.1982°
Arg. of periapsis
346.4139°
True anomaly
13.71085°
Mean anomaly
13.6852°
Eccentric anomaly
13.69802°
Mean motion
3.85671 °/min
Orbital period
93.34 mins
BSTAR
0.0007425
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