DECAYED
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MOVE-II, 43780 (Decayed)

Orbit data source: Space-Track

MOVE-II, 43780 was a payload satellite owned by TU Munchen (DE) in LEO that was launched on Mon, 03 Dec 2018 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.

Not visible in the next 10 days
Identifier
43780, 2018-099Y
Orbit
Decayed
Country
Flag of DEDE / GER
Related business
Manufacturer
TU Munchen
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
2018-12-03 (7 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
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: 10 months ago

TLE from 10 months ago
0 MOVE-II
1 43780U 18099Y   25194.80194206  .15913345  26116-5  37118-3 0  9995
2 43780  97.4526 273.8800 0018736 270.1080  89.8075 16.44566529363241
Epoch: 2025-07-13T19:14Z
TLE epoch observation values (Epoch: 2025-07-13T19:14:47.793Z)
Latitude
-0.00002°
Longitude
53.26092°
Altitude
156.921 km
Speed
7.812 km/s
True Right ascension
18h 15m 31s
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
08:19:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
162.719 km
Perigee altitude
138.255 km
Semi-major axis
6,528.624 km
Eccentricity
0.00187
Inclination
97.4526°
RAAN
273.88°
Arg. of periapsis
270.108°
True anomaly
90.0222°
Mean anomaly
89.8075°
Eccentric anomaly
89.91485°
Mean motion
4.11444 °/min
Orbital period
87.5 mins
BSTAR
0.00037118
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Computing Atmospheric mass density...

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