DECAYED
Showing default

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). 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.

Not visible in the next 10 days
Identifier
44412, 2019-038AC
Orbit
Decayed
Country
Flag of DEDE / GER
Related business
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 (6 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
Last TLE update: 1 year ago

TLE from 1 year 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
TLE epoch observation values (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 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
16:48:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
189.655 km
Perigee altitude
174.931 km
Semi-major axis
6,560.43 km
Eccentricity
0.00112
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
Orbital period
88.14 mins
BSTAR
0.0012178
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|