DECAYED
Showing default

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: 3 months ago

TLE from 3 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
18:47:46
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
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|