BEESAT 9, 44412 (Decayed)

Orbit data source: Space-Track

BEESAT 9, 44412 was a payload satellite owned by TUB (DE) in LEO that was launched on Fri, 05 Jul 2019 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). Payloads include a variety of satellites, spacecraft, and rockets 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.

Not visible in the next 10 days

BEESAT 9 details

Identifier	44412, 2019-038AC
Orbit	Decayed
Last TLE update	7 months ago
Origin	TUB (DE / GER)
Manufacturer	TUB
Mission	Decayed Amateur Technology
Bus & Motor	CUBESAT 1U, Unknown motor
Mass	1 kg wet, 1 kg dry
Launch date (UTC)	2019-07-05 (5 years ago)
Launch vehicle	SOYUZ-2-1B
Launch site	Vostochny Cosmodrome (VOSTO)
Object type	Payload Rocket body Debris
Shape & HBR	Box, 0.1 m
Radar Cross Section	0.015 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 7 months ago

0 BEESAT 9
1 44412U 19038AC  24155.76593309  .06929895  26845-5  12178-2 0  9994
2 44412  97.6577 163.7388 0011222 223.0270 137.0148 16.32636485272726

Epoch: 2024-06-03T18:22Z

Definitive object data (Epoch: 2024-06-03T18:22:56.618Z)

Latitude	-0.00008°
Longitude	-4.69436°
Altitude	194.091 km
Speed	7.787 km/s
True Right ascension	10h 54m 57s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	189.655 km
Perigee altitude	174.931 km
Semi-major axis	6,560.43 km
Eccentricity	0.0011222
Inclination	97.6577°
RAAN	163.7388°
Arg. of periapsis	223.027°
True anomaly	137.10239°
Mean anomaly	137.0148°
Eccentric anomaly	137.0586°
Mean motion	4.08455 °/min
BSTAR	0.0012178
Orbital period	88.14 mins