DECAYED
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MICRODRAGON, 43935 (Decayed)

Orbit data source: Space-Track

MICRODRAGON, 43935 was a payload satellite owned by VNSC (JP) in LEO that was launched on Fri, 18 Jan 2019 UTC via an EPSILON launch vehicle from the Kagoshima Space Center University Of Tokyo (KSCUT). 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
43935, 2019-003D
Orbit
Decayed
Country
Flag of JPJP / JPN
Related business
Flag of VNNational Satellite Center, Vietnam Academy of Science and Te (VN)
Manufacturer
VNSC
Mission
Decayed Civil Technology
Bus & Motor
MICRODRAGON, Unknown motor
Mass
50 kg wet, 50 kg dry
Launch date (UTC)
2019-01-18 (7 years ago)
Launch vehicle
EPSILON
Launch site
Kagoshima Space Center University Of Tokyo (KSCUT)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
0.514 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 year ago

TLE from 1 year ago
0 MICRODRAGON
1 43935U 19003D   24275.26385918  .16170828  23408-5  14762-3 0  9997
2 43935  97.0439 293.7887 0009366 285.9496  74.0778 16.51424394318676
Epoch: 2024-10-01T06:19Z
TLE epoch observation values (Epoch: 2024-10-01T06:19:57.433Z)
Latitude
-0.00002°
Longitude
-171.68068°
Altitude
137.196 km
Speed
7.825 km/s
True Right ascension
19h 35m 09s
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
23:20:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
138.462 km
Perigee altitude
126.267 km
Semi-major axis
6,510.501 km
Eccentricity
0.00094
Inclination
97.0439°
RAAN
293.7887°
Arg. of periapsis
285.9496°
True anomaly
74.18104°
Mean anomaly
74.0778°
Eccentric anomaly
74.12942°
Mean motion
4.13163 °/min
Orbital period
87.13 mins
BSTAR
0.00014762
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